System and method for forming a low temperature cured ceramic coating for elevated temperature applications

ABSTRACT

A method for forming an elevated temperature durable coating on a surface of a substrate includes applying an aqueous slurry comprising lithium silicate, sodium silicate, potassium silicate, zirconia powder, a fibrous agent, and a magnetic powder to a surface of a substrate in one or more layers of substantially uniform thickness to form a coating. A substantially controlled humidity environment is maintained during application of the aqueous slurry and the coating is ambient dried for a period. A drying agent is applied to the coating and formation of a dry crust is prevented on the coating during ambient drying. After the period, the coating is heat cured.

TECHNICAL FIELD

This invention relates generally to the field of ceramic coatings and,more specifically, to a method and system for forming a low temperaturecured ceramic coating for elevated temperature applications.

BACKGROUND

Ceramic coatings are often applied to jet engine and exhaust componentsfor thermal protection and energy absorption. Ceramic coatings are oftenformed by applying water-diluted, cement-based ceramic slurries,followed by ambient environment evaporation of the water of solution andelevated temperature curing of the cement to remove water of hydration.The cements are typically silicates of alkali metals and are used tobind together the appropriate ceramic oxides and energy absorbingfillers. The cements may also function as a primer to adhere the coatingto a metallic, ceramic or other substrate.

Most ceramic coatings are cured at temperatures of 1,000° Fahrenheit orgreater. Ceramic coatings that are applied under normal, ambientconditions and cured at low temperatures tend to crack and fail. Lowtemperature curable ceramic coatings, with or without a drying controlagent, may also crack and fail if applied and cured rapidly.

SUMMARY

In accordance with one embodiment of the present invention, a system andmethod for forming a low temperature cured ceramic coating for elevatedtemperature environments is provided that substantially eliminates orreduces disadvantages and problems associated with previously developedsystems and methods.

In accordance with one embodiment of the present invention, a method forforming an elevated temperature durable coating on a surface of asubstrate includes applying an aqueous slurry comprising lithiumsilicate, sodium silicate, potassium silicate, zirconia powder, afibrous agent, and a magnetic powder to a surface of a substrate in oneor more layers of substantially uniform thickness to form a coating. Asubstantially controlled humidity environment is maintained duringapplication of the aqueous slurry and the coating is ambient dried for aperiod. A drying agent is applied to the coating and formation of a drycrust is prevented on the coating during ambient drying. After theperiod, the coating is heat cured.

In accordance with another embodiment of the present invention, a heatresistant component for high temperature applications includes a coatingcomprising matrix materials, binder materials, strengthener materials,and magnetic fillers applied in one more substantially uniform thinlayers to a component. The coating is applied in a substantiallycontrolled humidity environment and dried for a period betweenapplication of each of the one or more thin layers. A drying agent isapplied to the coating and the coating and drying agent are heat curedfor a period.

Technical advantages of one or more embodiments of the present inventioninclude providing a heat resistant ceramic coating and method for hightemperature applications that includes applying an aqueous slurry and adrying agent to the substrate in a substantially controlled humidityenvironment to form a coating. After application of the aqueous slurryand drying agent, the coating is heat cured. Thus, a more uniformlycured coating with reduced drying stresses is provided.

Another technical advantage of one or more embodiments of the presentinvention includes providing a heat resistant, erosion resistant,ceramic coating which is substantially less susceptible to blisters,cracking, and shrinkage. More specifically, a ceramic coating isprovided that does not develop large cracks and subsequently disbondsfrom the substrate. Moreover, the resultant coating forms a solidprotective layer that is resistant to high humidity degradation orblistering after exposure to temperatures above 1,000° Fahrenheit. Andlongevity of substrates subjected to elevated temperatures is improved,reducing repair and/or replacement costs.

Other technical advantages of one or more embodiments of the presentinvention include providing a method for forming an elevated temperaturedurable coating on a surface of a substrate that includes applying anaqueous slurry and a drying agent to form a coating while maintaining asubstantially controlled humidity environment during application of thecoating. In this way, a low-cost method for providing a durable coatingon a surface of a substrate for use in elevated temperature environmentsis provided that can be applied to ceramic, titanium, and othersubstrates. The coating is heat cured and the resultant coating providesa moisture-resistant protective coating typically allowing small cracksof less than ten millimeters when exposed to elevated temperatureenvironments, thereby allowing the coating to tolerate strain withoutdisbanding from the substrate.

Other technical advantages are readily apparent to one skilled in theart from the following figures, descriptions, and claims. Moreover,some, all, or none of the above technical advantages may be included inthe various embodiments of the present invention.

BRIEF DESCRIPTION OF THE DRAWINGS

For a more complete understanding of the present invention and itsadvantages, reference is now made to the following description, taken inconjunction with the accompanying drawings, in which:

FIG. 1 illustrates an elevated temperature durable ceramic coating inaccordance with one embodiment of the present invention; and

FIG. 2 is a flowchart illustrating a method for forming the elevatedtemperature durable ceramic coating in accordance with one embodiment ofthe present invention.

DETAILED DESCRIPTION OF THE INVENTION

FIG. 1 illustrates a heat resistant component for elevated temperatureapplications of 1,000° Fahrenheit or greater in accordance with oneembodiment of the present invention. Component 10 may be a jet enginecomponent, exhaust component, or other suitable component. As usedherein, a heat resistant component is a component that may be used inelevated temperature environments. As used herein, an elevatedtemperature environment generally means temperatures at or exceeding950° to 1,000° Fahrenheit.

Component 10 includes component substrate 12, one or more layers ofaqueous slurry 14 (which form coating 15), and one or more layers ofdrying modification agent 16. Component substrate 12 may comprise thesurface of a jet engine component, a surface of an exhaust component, orother surface suitable for coating. Component substrate 12 may bepre-prepared for coating by, for example, cleaning, brushing, orotherwise prepared to enhance mechanical and chemical adhesion with theaqueous slurry 14 and drying modification agent 16.

As described in more detail below, an aqueous slurry is applied tocomponent substrate 12 in one or more thin layers 14 of substantiallyuniform thickness. A thin layer may be a layer between two to fivethousandths of an inch in thickness. As used herein, substantiallyuniform thickness means each of the one or more layers have a thicknessvariation of less than two thousandths of an inch in thickness. As usedherein, each means all of at least a subset. In one embodiment of thepresent invention, between twenty-five to fifty layers 14 of aqueousslurry are applied to component substrate 12, resulting in an overallthickness of approximately fifty thousandths of an inch. Layers 14 formcoating 15.

As described in more detail below, aqueous slurry 14 comprises matrixmaterials, binder materials, strengthener materials, and a magneticfiller. The matrix materials bind together appropriate ceramic oxidesand energy absorbing fillers in the resultant coating. The matrixmaterials may be silicates of alkali metals, cements, a combination oftwo, or otherwise suitable matrix materials. The binder materials adherethe coating to the component substrate. The strengthener materials,provide improved resistance to cracking and may comprise fibrous agents,glass frit, corderite glass, or other suitable strengthener materials.The magnetic filler provides desired electrical, magnetic, and othercharacteristics in the resultant coating. Magnetic fillers may comprise,for example, iron oxide, iron powder, or other suitable fillers.

In a particular embodiment, aqueous slurry 14 comprises lithiumsilicate, sodium silicate, potassium silicate, zirconia powder, afibrous agent, and a magnetic powder. In this embodiment, the watercontent of aqueous slurry 14 is controlled to between 15% and 20% byweight. Lithium silicate is present within the range of from about 5% toabout 20% by weight. Sodium silicate is present within the range of fromapproximately 5% to 20% by weight. Potassium silicate is present withinthe range of from approximately 5% to 20% by weight. Zirconia powder ispresent within the range of from approximately 10% to 20% by weight. Afibrous agent is present within the range of from approximately 2% to10% by weight. Magnetic powder is present within the range ofapproximately 40% to 75% by weight. Other suitable materials andproportions may be used.

The materials are mixed within an aqueous vehicle to provide a slurry ofthe insoluble dispersed zirconia powder, fibrous agent and magneticpowder and the water-soluble lithium, sodium, and potassium silicates.The majority of the water may be introduced as a component of thesilicates, which are commercially available in aqueous form under thetrade names AREMCO 516B, 516BT, and 516T from AREMCO PRODUCTS, INC.These materials typically have a water content of approximately 35% to70% by weight. The remaining components may be added as dry powders,allowing for the addition of a small amount of water to maintain thewater content between 15-20% by weight.

The zirconia powder has a particle size within the range of about 0.1 to20 micrometers. In one embodiment, the zirconia powder is zirconiumoxide with a particle size between about 0.3 and 3 micrometers. Thefibrous agent may be glass frit or corderite glass or other suitablefibrous agent. In one embodiment, the fibrous agent has an averageparticle size between about 1 and 25 micrometers. Suitable magneticfillers include iron oxide, iron powder, and similar magnetic powdersand particles.

In one embodiment, zirconia may be substituted for magnetic powder, forexample, to modify the magnetic signature of the resultant coating. Thefibrous agent may be employed as a strengthener and may be substitutedby short metallic fibers, or short ceramic fibers. As used herein, shortmeans a length that will prevent nesting or clumps and clogging aspraying nozzle. Generally, a short fiber has an aspect ratio ofapproximately 2:1 to 3:1, or 1 to 20 microns.

Other suitable substitutions may also be made to achieve varyingperformance characteristics of the resultant coating. For example, for astricter thermal barrier, more zirconia may be used. Other material maybe used for other needs, for example black powder for a black color tothe coatings.

The ingredients are uniformly mixed to form a slurry that may be appliedto a substrate as a uniform layer of a desired thickness. Theapplication of the coating is performed in a substantially controlledhumidity environment with the relative humidity being maintained between40% and 60%. As used herein, a substantially controlled humidityenvironment is an environment wherein the ambient relative humidity ismaintained between approximately 40% and 60%. Each layer may be allowedto dry for 30 to 90 minutes before the subsequent layer is applied.These conditions may help prevent the coating from prematurely crackingand peeling off the surface of the substrate.

Drying modification agent 16 includes a substantially uniform layerapplied to the coating 15. In one embodiment, drying modification agent16 comprises a mixture of glycerol and propylene glycol in substantiallyequivalent proportions, however, other suitable drying modificationagents may also be used. After application, drying modification agent 16diffuses into the outer surface layers of coating 15 and preventsformation of a dry crust or skin during a subsequent ambient environmentdrying process. Thus, a more uniform curing of the coating is achievedand drying stresses are reduced.

FIG. 2 illustrates a method for coating a surface of a substrate inaccordance with one embodiment of the present invention. The methodbegins at step 100, wherein the substrate to be coated is prepared. Suchpreparation may involve roughening the surface by mechanical means orapplying a rough metallic layer by flame or plasma spraying. Next atstep 105, the ambient environment humidity is controlled. In oneembodiment, the environmental relative humidity is maintained between40% and 60% during ambient drying. If the water is removed too fastblisters may form in the coating. If the water is removed too slowly,the coating may crack and shrink. Thus, controlling the humidity andheat in the environment where the coating is drying help form a moredurable protective coating. The relative humidity may be maintainedduring the entire process, during ambient steps of the process orotherwise.

Next at step 110, an aqueous slurry is prepared or obtained inaccordance with the composition as described above. Next at step 115, athin or other suitable layer of the aqueous slurry is applied to thesubstrate. The thin layer may be a layer between two to five thousandthsof an inch in thickness.

At step 120, the thin layer of aqueous slurry is allowed to dry for ashort time period. In one embodiment, the thin layer is allowed to dryfor approximately thirty to ninety minutes. The period may be suitablyshorter or longer. In addition, several layers may be applied betweenambient drying cycles. Next, at decisional step 125, a determination ismade whether additional thin layers of aqueous slurry are to be applied.If at decisional step 125 additional layers of aqueous slurry are to beapplied, the process proceeds along the Yes branch returning to step115, wherein an additional thin layer of aqueous slurry is applied.

If at decisional step 125 no additional thin layers of aqueous slurryare to be applied, the process proceeds along the No branch to step 130.At step 130, the one or more layers of aqueous slurry are allowed to dryfor a short period of time to achieve mechanical stability. In oneembodiment, the layers of aqueous slurry are allowed to dry forapproximately thirty to ninety minutes.

Next at step 135, a drying modification agent is applied to the topcoating of the one or more layers of aqueous slurry. In one embodiment,the drying modification agent consists of a mixture of glycerol andpropylene glycol in substantially equal proportion by volume. The dryingmodification agent soaks into the outer surface layer of the coating andmodifies the coating preventing the formation of a dry crust or skinduring the ambient environment dry process. This may result in moreuniform curing of the coating and decreases the drying stresses thattypically build up in ceramic coatings.

In one embodiment, the drying modification agent is applied in a layerapproximately one to two thousandths of an inch thick. In this and otherembodiments, the drying modification agent may be sprayed on but mayalso be brushed on. The drying modification agent may be operable tokeep the top layers and bottom layers drying at the same rate, producingan evenly dried area and preventing cracking and blistering.

Next at step 140, the coating is allowed to dry in the ambientenvironment. In one embodiment, the component is allowed to dry for aminimum of six hours after application of the drying agent. This timeperiod may be suitable varied or omitted. Next at step 145, theenvironment temperature is increased above ambient. In one embodiment,the temperature is increased at a rate of heating below 1.5° Fahrenheitper minute. As used herein, a rate of heating means the ramp up or downof the ambient temperature.

Next at step 150, the coating is heat cured. In one embodiment, thecoating is cured by maintaining the temperature of the ambientenvironment at about 350° Fahrenheit for a minimum of ninety minutes. Asused herein, about 350° Fahrenheit means a temperature range of between325° Fahrenheit and 375° Fahrenheit. Other suitable heat curedtemperatures above 125° Fahrenheit may be used. In one embodiment, totalcure time is approximately 12 hours. The resultant coating may yield aheat-resistant, erosion-resistant, protective ceramic coating. After thecoating is cured the process ends.

Although the method of FIG. 2 has been shown with specific steps in aspecific order, it will be understood that the steps may be performed ina different order as appropriate and other steps may be added or omittedas appropriate in keeping with the spirit of the present invention.

Although the present invention has been described with severalembodiments, various changes and modifications may be suggested to oneskilled in the art. It is intended that the present invention encompasssuch changes and modifications as fall within the scope of the appendedclaims.

1-23. (Cancelled)
 24. A heat resistant component for high temperatureapplications, comprising: a coating comprising one or more substantiallyuniform thin layers applied outwardly of a surface of a component in asubstantially controlled humidity environment; the layers eachcomprising a matrix material, binder material, strengthener material,and magnetic filler; the layers each dried for a period beforeapplication of a next one of the layers; and a drying agent applied tothe coating, and the coating and drying agent heat cured for a period.25. The component of claim 24, wherein the matrix materials comprise atleast one of a silicate of alkali metal and cement.
 26. The component ofclaim 24, wherein the silicate of alkali metal comprises lithiumsilicate, sodium silicate, and potassium silicate.
 27. The component ofclaim 24, wherein the strengthener materials comprise at least one ofglass frit, corderite glass, metallic fibers and ceramic fibers.
 28. Thecomponent of claim 24, wherein the magnetic filler comprises at leastone of iron oxide and iron powder.
 29. The heat resistant component ofclaim 24, wherein the coating and drying agent are heat cured at about350° Fahrenheit for a period of about ninety minutes.